EP1562151B1 - Dual-architecture microserver card - Google Patents
Dual-architecture microserver card Download PDFInfo
- Publication number
- EP1562151B1 EP1562151B1 EP04257148.9A EP04257148A EP1562151B1 EP 1562151 B1 EP1562151 B1 EP 1562151B1 EP 04257148 A EP04257148 A EP 04257148A EP 1562151 B1 EP1562151 B1 EP 1562151B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- section
- architecture section
- architecture
- closed
- engine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000004891 communication Methods 0.000 claims description 26
- 238000000034 method Methods 0.000 claims description 20
- 238000012544 monitoring process Methods 0.000 claims description 8
- 230000001413 cellular effect Effects 0.000 claims description 6
- 230000008569 process Effects 0.000 claims description 6
- 238000002485 combustion reaction Methods 0.000 claims description 5
- 230000009977 dual effect Effects 0.000 claims description 3
- 238000007405 data analysis Methods 0.000 claims 2
- 238000012423 maintenance Methods 0.000 description 20
- 230000008901 benefit Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 230000008439 repair process Effects 0.000 description 3
- 238000003860 storage Methods 0.000 description 3
- 239000003570 air Substances 0.000 description 2
- 239000012080 ambient air Substances 0.000 description 2
- 238000004458 analytical method Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 230000003993 interaction Effects 0.000 description 2
- 230000003287 optical effect Effects 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- KKIMDKMETPPURN-UHFFFAOYSA-N 1-(3-(trifluoromethyl)phenyl)piperazine Chemical compound FC(F)(F)C1=CC=CC(N2CCNCC2)=C1 KKIMDKMETPPURN-UHFFFAOYSA-N 0.000 description 1
- 102100024413 GTPase IMAP family member 5 Human genes 0.000 description 1
- 101150021309 Gimap5 gene Proteins 0.000 description 1
- 101001094649 Homo sapiens Popeye domain-containing protein 3 Proteins 0.000 description 1
- 101000608234 Homo sapiens Pyrin domain-containing protein 5 Proteins 0.000 description 1
- 101000578693 Homo sapiens Target of rapamycin complex subunit LST8 Proteins 0.000 description 1
- 102100027802 Target of rapamycin complex subunit LST8 Human genes 0.000 description 1
- 230000004913 activation Effects 0.000 description 1
- 230000003044 adaptive effect Effects 0.000 description 1
- 230000010267 cellular communication Effects 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000013480 data collection Methods 0.000 description 1
- 238000013500 data storage Methods 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000003745 diagnosis Methods 0.000 description 1
- 238000002405 diagnostic procedure Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 230000033001 locomotion Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 230000029305 taxis Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G07—CHECKING-DEVICES
- G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
- G07C5/00—Registering or indicating the working of vehicles
- G07C5/08—Registering or indicating performance data other than driving, working, idle, or waiting time, with or without registering driving, working, idle or waiting time
- G07C5/0841—Registering performance data
- G07C5/085—Registering performance data using electronic data carriers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
-
- G—PHYSICS
- G07—CHECKING-DEVICES
- G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
- G07C5/00—Registering or indicating the working of vehicles
- G07C5/008—Registering or indicating the working of vehicles communicating information to a remotely located station
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L63/00—Network architectures or network communication protocols for network security
- H04L63/04—Network architectures or network communication protocols for network security for providing a confidential data exchange among entities communicating through data packet networks
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L67/00—Network arrangements or protocols for supporting network services or applications
- H04L67/01—Protocols
- H04L67/02—Protocols based on web technology, e.g. hypertext transfer protocol [HTTP]
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L67/00—Network arrangements or protocols for supporting network services or applications
- H04L67/01—Protocols
- H04L67/02—Protocols based on web technology, e.g. hypertext transfer protocol [HTTP]
- H04L67/025—Protocols based on web technology, e.g. hypertext transfer protocol [HTTP] for remote control or remote monitoring of applications
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L67/00—Network arrangements or protocols for supporting network services or applications
- H04L67/01—Protocols
- H04L67/04—Protocols specially adapted for terminals or networks with limited capabilities; specially adapted for terminal portability
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L67/00—Network arrangements or protocols for supporting network services or applications
- H04L67/01—Protocols
- H04L67/12—Protocols specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L69/00—Network arrangements, protocols or services independent of the application payload and not provided for in the other groups of this subclass
- H04L69/30—Definitions, standards or architectural aspects of layered protocol stacks
- H04L69/32—Architecture of open systems interconnection [OSI] 7-layer type protocol stacks, e.g. the interfaces between the data link level and the physical level
- H04L69/322—Intralayer communication protocols among peer entities or protocol data unit [PDU] definitions
- H04L69/329—Intralayer communication protocols among peer entities or protocol data unit [PDU] definitions in the application layer [OSI layer 7]
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04W—WIRELESS COMMUNICATION NETWORKS
- H04W12/00—Security arrangements; Authentication; Protecting privacy or anonymity
- H04W12/03—Protecting confidentiality, e.g. by encryption
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/80—Diagnostics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/11—Purpose of the control system to prolong engine life
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/40—Type of control system
- F05D2270/44—Type of control system active, predictive, or anticipative
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/50—Control logic embodiments
- F05D2270/54—Control logic embodiments by electronic means, e.g. electronic tubes, transistors or IC's within an electronic circuit
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/70—Type of control algorithm
- F05D2270/708—Type of control algorithm with comparison tables
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y04—INFORMATION OR COMMUNICATION TECHNOLOGIES HAVING AN IMPACT ON OTHER TECHNOLOGY AREAS
- Y04S—SYSTEMS INTEGRATING TECHNOLOGIES RELATED TO POWER NETWORK OPERATION, COMMUNICATION OR INFORMATION TECHNOLOGIES FOR IMPROVING THE ELECTRICAL POWER GENERATION, TRANSMISSION, DISTRIBUTION, MANAGEMENT OR USAGE, i.e. SMART GRIDS
- Y04S40/00—Systems for electrical power generation, transmission, distribution or end-user application management characterised by the use of communication or information technologies, or communication or information technology specific aspects supporting them
- Y04S40/18—Network protocols supporting networked applications, e.g. including control of end-device applications over a network
Definitions
- the present disclosure generally relates to integrated Internet systems and, more particularly, relates to the provision of an internet portal on board a deployed product.
- On-demand maintenance usually when a product breaks
- scheduled maintenance based upon the best estimate of a manufacturer as to when something will wear out with normal usage
- condition based maintenance maintenance that occurs when maximum usage is obtained from a part but just prior to part failure.
- On demand maintenance is self-explanatory. It is when a component fails and has to be repaired or replaced. This normally occurs as an end result of its operators not understanding its component life or the conditions of its use, and the highest costs, both physical and lost time, are associated with it.
- Scheduled maintenance is less costly but can be very wasteful. Depending upon the usage of a product, one may be replacing parts that still have a significantly useful life.
- condition-based maintenance is the holy grail of maintenance in many industries. If a manufacturer or service organization can accurately ascertain the maximum life of a component based upon actual wear, tear, and usage, it could then allow for the optimized, just-in-time servicing and replacement of that component, thereby allowing for the user to gain maximum product life and to schedule the replacement at a non-critical time. As a result, a manufacturer utilizing condition based maintenance could better plan its spares production and save millions of dollars in unnecessary production, warehousing and inventory taxes.
- EDUs engine data units
- EEC electronic engine control
- a number of industries normally attempt to gather product usage intelligence through manual inspections and, more recently, laptop computer downloads performed concurrently with scheduled or on-demand maintenance service calls. This is normally accomplished by one of two methods: sending a service person to the product, bringing the product to a service center, or both.
- Examples of the former include products with fixed installations, such as elevators, HVAC systems, nuclear power plants and large home appliances. Examples of the latter include automobiles, small home appliances, home electronics equipment, lawn-mowers, or anything small enough to be easily carried or shipped. Both methods are inefficient and result in significant down time.
- EP1316908 describes an integrated system for monitoring a deployed product on a movable platform, gathering data about the deployed product, and disseminating the data about the deployed product.
- the system includes a server located on the movable platform capable of communication with the server from a remote location.
- the server communicates with a source of data about the deployed product.
- the system further includes a portal into which data gathered by the server may be downloaded and with which one can upload information to the server.
- US 6115656 describes a method for recording and reporting fault information pertaining to various components of an aircraft, involving recording a diverse plurality of information output from various line replaceable units (LRU's) and other components of the aircraft during takeoff, flight and landing through the use of a bulk storage device, such as an optical quick access recorder (OQAR), on an electronic medium. The electronic medium is then removed from the aircraft after landing and read by an appropriate apparatus.
- LRU's line replaceable units
- OQAR optical quick access recorder
- WO 0180494 describes a remote control and a monitoring system using an Internet, which includes a host part installed on a position wherein a controlled object is located for inputting an image data, a sound data and a sensing data to output a control signal, a server part for storing the image data, the sound data and the sensing data received from the host part and transmitting the stored control signal to the host part, and a web client part for receiving the image data, the sound data and the sensing data stored in the server part in a programmed form, displaying thereof by a web browser, and transmitting the control signal to the server part.
- EP 1175062 describes a control system that allows a user to access an input/output device over a communication network using a web browser.
- the system includes an Internet web site between the network and the input/output module.
- the web site runs from an Ethernet board coupled directly to the input/output module back plane and includes a HTTP protocol interpreter, an input/output module, a TCP/IP stack, and an Ethernet board kernel.
- the web site provides access to the input/output module by a user at a remote location through the Internet.
- the web site translates the industry standard Ethernet, TCP/IP and HTTP protocols used on the Internet into data recognizable to the input/output module. Using this interface, the user can input or retrieve all pertinent data regarding the operation of the input/output device.
- US 6487717 describes a system and method for controlling an engine or machine at a remote unit from a central office.
- An interface connected to a computer of the engine or machine controller is integrated with a communications module that is configured to establish communications with a World Wide Web server on the Internet.
- a similar system is established at the location of the central office connected to a computer controlled by a fleet owner/operator, for example.
- the fleet owner can upload machine control data or machine control application software to an intermediate digital file storage maintained by the Web server via the Internet.
- an electronic controller according to claim 23.
- a system 10 is presented which is capable of monitoring a deployed product, gathering data about the deployed product, and disseminating the data to interested parties. It is also capable of monitoring and restricting access to its data, and can accept data for storage or integration within the product itself, such as firmware revision updates.
- the term "deployed product” has broad applicability and refers to any product, component, or system on a variety of machines including, but not limited to a vehicle, a HVAC system, or an elevator/escalator system such as a propulsion system on a vehicle, a compartment of a vehicle, or a braking system for a vehicle, wherein the vehicle is any one of a number of movable devices including aircraft and elevator cars.
- the system 10 includes a server 12 located on the deployed product or movable platform 14.
- the movable platform 14 may be a boat, an airplane, a spacecraft, an automobile, a truck, or any other entity that is movable with an airplane being depicted for ease of understanding.
- the server 12 may monitor the condition of and/or gather data about the deployed product in a number of ways.
- the server 12 may be connected to or integrated with a vehicle data storage unit 16 which contains data about the deployed product.
- the server 12 may also be connected to a video camera 18, such as video web camera, to provide pictures, in real-time or on a delayed basis, of the deployed product.
- the server 12 may be connected to a number of sensors 20, such as a vibration sensor or a temperature sensor, which provide additional or environmental information about the condition of the deployed product.
- the server 12 may be programmed in any suitable language known in the art to gather data about the deployed product and present the data to interested parties in a desired format.
- the server 12 may be used to host a web page which provides information about one or more deployed products on the movable platform.
- the web page may have a menu which allows an interested party to gain access to gathered data about a particular deployed product.
- the data about the deployed product(s) may be organized on the server 12 and presented in any desirable format or manner.
- the server 12 may also be programmed to allow an interested party to carry out diagnostic operations on the deployed product(s) and/or to upgrade software associated with the deployed product(s).
- the web page may have an IP address available for various Internet protocols including, but not limited to, HTTP, FTP, SMTP, UDP, ECHO, SSH, TELNET, NAMESERVER, BOOT PS, BOOT PC, TFTP, KERBEROS, POP3, NNTP, IMAP, SNMP, BGP, IMAP3, LDAP, and HTTPS.
- the server 12 may be provided with a local USB or other communications port 22 for direct hook-up.
- a mechanic or engineer could then gain access to the server 12 by hooking up a promtop, laptop computer or another device 23 such as a video borescope or a bar code reader to the communications port 22.
- Other examples of communication ports through which access may be gained to server 12 include wireless peer-to-peer communication links.
- the mechanic or engineer could then conduct a desired diagnostic operation or even fix a problem with the deployed product.
- any passenger on board the deployed product 14 could use his or her own computer device 23 to access the server 12 and thus the Internet 25, again as will be described in further detail herein.
- the server 12 may comprise any suitable computer or processing unit known in the art.
- the server 12 may be a hand-held sized microserver using a Linux-based operating system or, as will be described in further detail herein, may be a card adapted to be installed in a larger computer device. Further, the server 12 may be provided with its own web address, a firewall, and security protocols known only to selected individuals, such as the manufacturer of the deployed product.
- the server 12 is capable of being accessed by interested parties via a portal 24 and the Internet or world wide web 25.
- the server 12 may have a communications device, such as a modem built within it to allow communication between the server 12 and the portal 24.
- the communication device may allow for radio frequency communications such as cellular communication, satellite communication, and/or wireless communication between the server 12 and the portal 24.
- communications between the server 12 and the portal 24 may be achieved by optical means such as an infrared link.
- the portal 24 is hosted by an external server which may be any suitable server known in the art.
- the server hosting the portal 24 also has appropriate communication means associated with it to allow it to gain access to and be accessed by the server 12.
- Data gathered by and stored on the server 12 may be downloaded to the portal 24 as desired.
- the server 12 may be programmed to periodically download data to the server hosting the portal 24 or to download data on specific events such as when an aircraft lands or when a truck or automobile reaches a particular destination.
- the server 12 may also download data to the portal 24 upon the activation of a switch by an operator onboard the moving platform.
- the portal server may upload data to the microserver, such as product firmware revisions or technical manuals for access by interested parties.
- the server may include an antenna 27 or the like to facilitate such wireless communication.
- the portal 24 may be provided with a number of software tools called gadgets to automatically analyze, organize, and sort the data which has been received from the server 12.
- the data is preferably sorted so that different communities gain access to different portions of the data. For example, actual and potential customers of a vendor of a deployed product may form one community and have access to certain data, while support engineers and product designers may form a second community and have access to another form of the data.
- the portal 24 offers great flexibility as to how and to whom the data is disseminated.
- the portal 24 provides virtual shared spaces which allow for the common space posting and access of information about a deployed product in a shared awareness between customers, support engineers, field operatives, and even product designers.
- the portal 24 may also be designed to provide chat rooms, bulletin boards, and on-line meeting capabilities where interested parties can communicate with each other.
- One of the advantages to using the portal 24 is that its functionality can be carried out in a secure, user friendly, web-based environment. Members of a particular community can log in by presenting an identification and/or a password and gain access to current information about a deployed product.
- Another advantage to using the portal 24 is that it can be used to upload data, information, instructions, software, technical publications, diagnostic programs, etc. to the server 12.
- an engineer can perform diagnostic tests on a deployed product from a remote location using the Internet.
- a service engineer working in the aircraft can gain access to a technical publication outlining how to repair a certain situation, for example, through the server 12.
- As the communication is two way, access, upload, download, and execution of all such information and data can be performed at the deployed product or remote locations.
- Access to the portal 24 may be gained in a number of different ways by a variety of devices as described below.
- an interested party can communicate with the portal 24 through his/her personal computer 38 and the web browser on the computer 38.
- the computer 38 may be a PC workstation at an office of a user or a laptop or PC at the home of a user. Even a computer 40 in an Internet cafe may be used to gain access to the portal 24.
- a wireless PC tablet 36 on the shop floor of a manufacturer of the deployed product may also be used to communicate with the portal 24.
- the portal 24 may also be in communication with the internal network 30 of the manufacturer of or a vendor of the deployed product.
- a secure data pipe 32 may be used for crawlers for automated data exchange.
- the portal 24 may communicate with the internal network 30 via a wireless PDA.
- the system 10 may also be configured to allow the internal network 30 to communicate directly with the server 12 via the Internet by dialing up the web address for the server 12.
- a firewall may be provided between the internal network 30 and the server 12.
- the system 10 of the present disclosure has broad applicability and can be used for a wide variety of purposes.
- the system 10 can be used by an engineer working for a manufacturer of the deployed product to gain access to the server 12 and to then carry out a diagnostic operation or a fix on a particular deployed product. All of this can be carried out while the movable platform 14 is in motion and in a location remote from the engineer, thus avoiding having to return a deployed product to a manufacturer for diagnosis and repair.
- the system 10 may also be used to check the status of a deployed product.
- an operator of a fleet of airplanes having a network 30 may contact the server 12 on a particular airplane, either directly or through the portal 24, and learn the location of and the status of that airplane.
- a manufacturer of a jet engine may access the server 12 through its network, again either directly or through the portal 24, to ascertain the condition of a particular jet engine or a particular component on the jet engine to determine when that engine or component may require to servicing, and to collect data in determining product and fleet averages for improved product design and support. This can save the manufacturer unnecessary warranty, maintenance wear, and spare parts production costs.
- the server 12 may be installed in the cabin of an aircraft, by using existing test ports already wired into the engine/airframe. Once installed, the server 12 generates a local wireless intranet in and around the deployed product capable of operating in conjunction with, or independent from, the Internet.
- the microserver 12 can act as a coordinating server in communication with other computing devices, servers, and systems onboard the deployed product.
- an engine 50 of an aircraft is depicted, such as a gas turbine engine used for propulsion.
- a fan case 51 surrounds a compressor section 52, a combustion section 54, and a turbine section 56.
- the compressor section 52 ingests ambient air, compresses that air and directs the compressed air to the combustion section 54 where it is combined with fuel and ignited.
- the resulting combustion gases which are very hot and rapidly expanding, are directed to the turbine section 56 where they impart force to rotatable blades.
- the blades rotate and cause a shaft assembly 58 extending through the engine to rotate as well. Since blades of the compressor section 52 are mounted to the same shaft assembly 58, the compressor section 52 rotates as well, thereby drawing in more ambient air and perpetuating the engine cycle.
- Operation of the engine 50 is controlled and monitored by an electronic controller or control box 62, known by different acronyms within the industry such as, for example, a FADEC (Full Authority Digital Engine Control) or an EEC (Electronic Engine Control).
- a controller 62 receives data from the engine by way of hard-wired inputs, wireless inputs, RF ID tags and the like, calculates correctional signals to optimize operation, and transmits control signals back to the engine.
- the means for controlling the engine may employ any known technology, but generally performs as an electronic fuel control or injector taking power and throttle commands/signals from the cockpit and adjusting engine control to provide the desired power.
- the EEC or other electronic control may include a plurality of cards or boards, including a motherboard, slidably mounted in a rack of the EEC.
- the cards/boards receive inputs from the cockpit and various engine sensors, and output signals to various valves and controls of the engine to effectuate its operation.
- the controller 62 may include an antenna 63 to facilitate wireless communication.
- the software or algorithms used by the engine 50 in doing this may be propriety, or it may otherwise be desirable to keep such information from outside observers, it is necessary to ensure such software is executed in a safe or closed capacity.
- this is relatively easy to accomplish in that to gain access to the software, a user had to be hardwired to the controller 62.
- the present disclosure provides a microserver on the engine 50 and thus enables wireless communication with remote computing devices, a system is provided to more internally protect the proprietary software.
- the dual-architecture card 64 of the present disclosure is depicted as the mechanism by which such protection is accomplished.
- the dual-architecture card 64 which may be mounted directly within the EEC 62 along with other electronic cards, includes a closed architecture section 66 and an open architecture section 68 connected by a high security connection 70.
- Engine control algorithms are processed by the closed architecture section 66 for operation of the engine 50, and only data processed or "cleaned" by the closed architecture section 66 is then communicated to the open architecture section 68 for access by interested parties.
- the closed architecture section 66 may include one or more processors 72 and one or more input/output devices 74.
- the closed architecture section 66 may include a smart signal conditioner 76 having various microprocessors such as predictive maintenance chips or modules, diagnostic modules, compressor stall analysis modules, etc. which run proprietary, embedded engine-specific algorithms that process engine data received from engine sensors 75.
- the chips and modules are hard-coded into the smart signal conditioner 76 so as to render their algorithms inaccessible to other operators, such as original equipment manufacturers (OEMs), with data access.
- OEMs original equipment manufacturers
- the closed architecture section 66 can then feed calculated data and signals back into engine controller 62 and other aircraft systems such as hydraulics, landing gear, flaps, and mission profile, for real-time mission adaptive processing and performance optimization.
- the open architecture section 68 may include one or more processors 78 and a microserver 80.
- the microserver 80 generates a wireless system or intranet about the aircraft or engine 50 enabling communication with the Internet as by a local area network (LAN) 82, cellular network 84, or satellite 86.
- the microserver may host a webpage enabling remote computing devices 88 to log into the webpage by way of the Internet 89 and receive the processed data.
- Any number of remote computing devices may be employed such as, but not limited to, desktop computers 90, laptop computers 92, personal digital assistants 94, cellular phones 96, and wireless PC tablets 98.
- a user in a location remote from the airborne aircraft such as in an office, home, or maintenance facility, can gain access to certain engine data while maintaining the proprietary nature of certain engine algorithms.
- the engine 50 is able to do so due to the dual architecture card 64 and its smart signal conditioner 76 and high security connector 70 between the open architecture section 68 and closed architecture section 66.
- the closed architecture section 66 includes its own microserver 100.
- the microserver 100 may host its own webpage, and by way of a secure internet connection, enable owners of the engine to gain access to the raw engine data, or modify the proprietary algorithm. Such a system may enable software upgrades from remote locations while still preventing unwanted access.
Landscapes
- Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Signal Processing (AREA)
- Computer Security & Cryptography (AREA)
- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Computing Systems (AREA)
- General Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Medical Informatics (AREA)
- General Health & Medical Sciences (AREA)
- Computer Hardware Design (AREA)
- Health & Medical Sciences (AREA)
- Mechanical Engineering (AREA)
- Selective Calling Equipment (AREA)
- Debugging And Monitoring (AREA)
- Test And Diagnosis Of Digital Computers (AREA)
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
- Control Of Vending Devices And Auxiliary Devices For Vending Devices (AREA)
- Arrangements For Transmission Of Measured Signals (AREA)
- Computer And Data Communications (AREA)
- Financial Or Insurance-Related Operations Such As Payment And Settlement (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
- Information Transfer Between Computers (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US769427 | 1985-08-26 | ||
US10/769,427 US7167788B2 (en) | 2004-01-30 | 2004-01-30 | Dual-architecture microserver card |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1562151A2 EP1562151A2 (en) | 2005-08-10 |
EP1562151A3 EP1562151A3 (en) | 2005-11-16 |
EP1562151B1 true EP1562151B1 (en) | 2016-05-11 |
Family
ID=34679338
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP04257148.9A Active EP1562151B1 (en) | 2004-01-30 | 2004-11-18 | Dual-architecture microserver card |
Country Status (12)
Country | Link |
---|---|
US (3) | US7167788B2 (zh) |
EP (1) | EP1562151B1 (zh) |
JP (1) | JP4762556B2 (zh) |
CN (1) | CN1649348B (zh) |
AU (1) | AU2004226952A1 (zh) |
BR (1) | BRPI0405155A (zh) |
CA (1) | CA2486088A1 (zh) |
MX (1) | MXPA04012874A (zh) |
NZ (1) | NZ535744A (zh) |
RU (1) | RU2005102131A (zh) |
SG (3) | SG113544A1 (zh) |
TW (1) | TW200525367A (zh) |
Families Citing this family (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20060164239A1 (en) * | 2003-01-14 | 2006-07-27 | Loda David C | Shipping container and method of using same |
US7844385B2 (en) | 2004-01-28 | 2010-11-30 | United Technologies Corporation | Microserver engine control card |
US20060168090A1 (en) | 2005-01-07 | 2006-07-27 | United Technologies Corporation | Remote integrated subsystems in an aircraft or the like |
US8643507B2 (en) * | 2005-03-28 | 2014-02-04 | Gary G. Rodriguez | Vehicle-based threat detection system |
WO2006125014A2 (en) * | 2005-05-17 | 2006-11-23 | United Technologies Corporation | Personal wearable microserver |
US8341298B2 (en) | 2005-12-02 | 2012-12-25 | The Boeing Company | Scalable on-board open data network architecture |
EP2002402A1 (en) * | 2006-03-31 | 2008-12-17 | Snap-on Incorporated | In-vehicle diagnostic system with built-in browser capabilities |
US7854127B2 (en) * | 2006-10-24 | 2010-12-21 | United Technologies Corporation | Smart wireless engine sensor |
US7689327B2 (en) * | 2006-11-21 | 2010-03-30 | United Technologies Corporation | Microserver adapter for an avionics box |
US8565998B2 (en) * | 2006-11-27 | 2013-10-22 | United Technologies Corporation | Gas turbine engine having on-engine data storage device |
US8078354B2 (en) * | 2006-11-29 | 2011-12-13 | United Technologies Corporation | Global product management of a vehicle and a fleet of vehicles |
FR2917521B1 (fr) * | 2007-06-15 | 2009-10-02 | Airbus France Sa | Systeme informatique de maintenance d'un aeronef |
US8200376B2 (en) * | 2007-07-30 | 2012-06-12 | Symvionics, Inc. | Vehicle performance monitoring system with multi-level caching |
US7715943B2 (en) | 2008-03-07 | 2010-05-11 | United Technologies Corporation | Microserver for managing an assembly or repair of a product |
US20110140866A1 (en) * | 2008-03-26 | 2011-06-16 | Paul Raymond Scheid | Wireless aircraft maintenance log |
US8527240B2 (en) * | 2008-03-26 | 2013-09-03 | United Technologies Corporation | Wireless sensor assembly for an aircraft component |
US20090243854A1 (en) * | 2008-03-26 | 2009-10-01 | Paul Raymond Scheid | Wireless aircraft maintenance log |
US8140242B2 (en) * | 2008-05-22 | 2012-03-20 | United Technologies Corp. | Systems and methods involving multiplexed engine control signals |
US20100048202A1 (en) * | 2008-08-25 | 2010-02-25 | Beacham Jr William H | Method of communicating with an avionics box via text messaging |
US20100242492A1 (en) * | 2009-03-30 | 2010-09-30 | Honeywell International Inc. | Distributed engine control systems and gas turbine engines |
US9092029B2 (en) * | 2009-04-21 | 2015-07-28 | Hamilton Sundstrand Corporation | Vehicle monitoring system |
US8054204B2 (en) * | 2009-05-29 | 2011-11-08 | United Technologies Corporation | Method for remotely updating wireless sensors |
US8509963B1 (en) * | 2009-07-23 | 2013-08-13 | Rockwell Collins, Inc. | Remote management of aircraft computer systems |
FR2955185B1 (fr) * | 2010-01-11 | 2012-09-21 | Sagem Defense Securite | Dispositif de controle d'un moteur d'aeronef |
US8335609B2 (en) * | 2010-01-25 | 2012-12-18 | United Technologies Corporation | Method and system for exposing and recording embedded avionics data |
US9092920B2 (en) | 2012-03-27 | 2015-07-28 | United Technologies Corporation | System and method for managing a vehicle and a fleet of vehicles |
US9388744B2 (en) * | 2012-03-30 | 2016-07-12 | General Electric Company | Distributed gas turbine engine control system with remote interface units |
US9932121B2 (en) * | 2012-06-22 | 2018-04-03 | United Technologies Corporation | Turbomachine flow stability enhancement device control |
US10590855B2 (en) * | 2015-02-03 | 2020-03-17 | United Technologies Corporation | Distributed electrical architecture for a gas turbine engine |
US9550583B2 (en) * | 2015-03-03 | 2017-01-24 | Honeywell International Inc. | Aircraft LRU data collection and reliability prediction |
US10626803B2 (en) * | 2015-10-22 | 2020-04-21 | United Technologies Corporation | Apparatus and method for controlling and monitoring an electro-hydraulic servovalve |
TWI567567B (zh) * | 2015-12-25 | 2017-01-21 | 英業達股份有限公司 | 微型伺服器 |
EP3287990B1 (en) | 2016-08-25 | 2020-09-30 | Airbus Operations GmbH | Data acquisition system and methods for data acquisition |
FR3064602B1 (fr) * | 2017-03-29 | 2019-06-07 | Airbus Operations | Mode de fonctionnement degrade d'un groupe propulseur d'aeronef permettant le deplafonnement d'une consigne de poussee |
CN110321235B (zh) * | 2019-07-08 | 2021-03-16 | 北京可信华泰信息技术有限公司 | 基于双体系架构的可信计算平台的系统交互方法和装置 |
CN112181759A (zh) * | 2020-09-04 | 2021-01-05 | 广东电力信息科技有限公司 | 一种微服务性能监视及异常诊断的方法 |
Family Cites Families (55)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA961920A (en) * | 1970-10-20 | 1975-01-28 | John F. Reuther | System and method for operating industrial gas turbine apparatus and gas turbine electric power plants preferably with a digital computer control system |
CA2096374C (en) * | 1992-05-18 | 2006-08-08 | Michael A. Sandifer | Computer aided maintenance and repair information system for equipment subject to regulatory compliance |
US5445347A (en) * | 1993-05-13 | 1995-08-29 | Hughes Aircraft Company | Automated wireless preventive maintenance monitoring system for magnetic levitation (MAGLEV) trains and other vehicles |
US5828969A (en) * | 1995-06-22 | 1998-10-27 | Canadian Digital Photo/Graphics Inc. | Process for use with aircraft repairs |
US5884202A (en) * | 1995-07-20 | 1999-03-16 | Hewlett-Packard Company | Modular wireless diagnostic test and information system |
US6522867B1 (en) * | 1995-11-14 | 2003-02-18 | Harris Corporation | Wireless, frequency-agile spread spectrum ground link-based aircraft data communication system with wireless unit in communication therewith |
US6047165A (en) * | 1995-11-14 | 2000-04-04 | Harris Corporation | Wireless, frequency-agile spread spectrum ground link-based aircraft data communication system |
FR2742897B1 (fr) * | 1995-12-22 | 1998-02-20 | Aerospatiale | Dispositif de surveillance d'un systeme complexe, notamment d'un aeronef |
US5931877A (en) * | 1996-05-30 | 1999-08-03 | Raytheon Company | Advanced maintenance system for aircraft and military weapons |
US6234176B1 (en) * | 1996-06-21 | 2001-05-22 | Integrated Medical Systems, Inc. | Data logger for transportable life support system |
US5931878A (en) * | 1996-08-09 | 1999-08-03 | Mindersoft, Inc. | Computerized prompting systems |
US6115656A (en) * | 1997-06-17 | 2000-09-05 | Mcdonnell Douglas Corporation | Fault recording and reporting method |
US6732191B1 (en) | 1997-09-10 | 2004-05-04 | Schneider Automation Inc. | Web interface to an input/output device |
US20050124337A9 (en) * | 1998-09-08 | 2005-06-09 | Tenzing Communications, Inc. | System and method for airborne passenger electronic communication |
US6141584A (en) * | 1998-09-30 | 2000-10-31 | Agilent Technologies, Inc. | Defibrillator with wireless communications |
US6112246A (en) * | 1998-10-22 | 2000-08-29 | Horbal; Mark T. | System and method for accessing information from a remote device and providing the information to a client workstation |
US6487717B1 (en) * | 1999-01-15 | 2002-11-26 | Cummins, Inc. | System and method for transmission of application software to an embedded vehicle computer |
US6154636A (en) * | 1999-05-14 | 2000-11-28 | Harris Corporation | System and method of providing OOOI times of an aircraft |
US6148179A (en) * | 1999-06-25 | 2000-11-14 | Harris Corporation | Wireless spread spectrum ground link-based aircraft data communication system for engine event reporting |
CN1251502C (zh) * | 1999-08-27 | 2006-04-12 | 诺基亚有限公司 | 用于数字视频广播的移动多媒体终端 |
US7020697B1 (en) * | 1999-10-01 | 2006-03-28 | Accenture Llp | Architectures for netcentric computing systems |
US6606546B2 (en) * | 1999-12-01 | 2003-08-12 | Sinex Holdings, Llc | Aircraft maintenance program manager |
US6487479B1 (en) * | 2000-01-07 | 2002-11-26 | General Electric Co. | Methods and systems for aviation component repair services |
US6742704B2 (en) * | 2000-01-21 | 2004-06-01 | American Express Travel Related Services Company, Inc. | Multiple-service card system |
US6370454B1 (en) * | 2000-02-25 | 2002-04-09 | Edwin S. Moore Iii | Apparatus and method for monitoring and maintaining mechanized equipment |
JP2003530746A (ja) * | 2000-04-10 | 2003-10-14 | ハネウェル・インターナショナル・インコーポレーテッド | 機内電子メール・システム |
KR100390530B1 (ko) | 2000-04-15 | 2003-07-04 | (주)디지털넷뱅크 | 인터넷을 이용한 원격 제어 및 모니터링 장치 및 방법 |
US20030093798A1 (en) * | 2000-07-10 | 2003-05-15 | Michael Rogerson | Modular entertainment system configured for multiple broadband content delivery incorporating a distributed server |
WO2002015582A1 (en) * | 2000-08-16 | 2002-02-21 | The Boeing Company | Method and apparatus for providing bi-directional data services and live television programming to mobile platforms |
AU2001289056A1 (en) * | 2000-09-11 | 2002-03-26 | Pinotage, Llc | System and method for obtaining and utilizing maintenance information |
JP2002091913A (ja) * | 2000-09-12 | 2002-03-29 | Techno Digital:Kk | 遠隔メンテナンスシステム、並びにこれに用いられるメンテナンス装置およびサポート装置 |
US6606055B2 (en) * | 2000-12-06 | 2003-08-12 | Harris Corporation | Phased array communication system providing airborne crosslink and satellite communication receive capability |
US7076532B2 (en) * | 2001-01-15 | 2006-07-11 | Ron Craik | System and method for storing and retrieving equipment inspection and maintenance data |
US6671589B2 (en) * | 2001-02-13 | 2003-12-30 | William Holst | Method and apparatus to support remote and automatically initiated data loading and data acquisition of airborne computers using a wireless spread spectrum aircraft data services link |
US7127409B2 (en) * | 2001-03-01 | 2006-10-24 | General Electric Company | Methods and systems for aviation nonconformance component management |
US6567729B2 (en) * | 2001-03-28 | 2003-05-20 | Pt Holdings Ltd. | System and method of analyzing aircraft removal data for preventative maintenance |
US20020160773A1 (en) * | 2001-03-29 | 2002-10-31 | Tenzing Communications, Inc. | Communications systems for aircraft including wireless systems |
US20020178751A1 (en) * | 2001-05-18 | 2002-12-05 | Moti Malek | Open gem tips |
US7610602B2 (en) | 2001-05-23 | 2009-10-27 | The Directv Group, Inc. | Method, system and computer program product for aircraft multimedia distribution |
US6990338B2 (en) * | 2001-06-11 | 2006-01-24 | The Boeing Company | Mobile wireless local area network and related methods |
US20030014426A1 (en) * | 2001-07-11 | 2003-01-16 | Gimbert Norman Wesley | System and method for communicating aircraft and aircraft engine information |
US20030032426A1 (en) * | 2001-07-24 | 2003-02-13 | Gilbert Jon S. | Aircraft data and voice communications system and method |
AU2002332850A1 (en) * | 2001-09-06 | 2003-03-24 | Airia Inc. | Method and system for providing an audio/video in-route entertainment system |
US20030085818A1 (en) * | 2001-09-07 | 2003-05-08 | Renton Joseph J. | System and method for acquiring, storing, processing and presenting data accumulated through an in-flight aircraft server |
US20030048471A1 (en) * | 2001-09-10 | 2003-03-13 | Lundgren Mark A. | System and method for providing in-flight computer printing services on an aircraft |
US20030064714A1 (en) * | 2001-10-02 | 2003-04-03 | Sanford William C. | Consolidated in-flight entertainment electronic system |
US20040206818A1 (en) * | 2001-12-03 | 2004-10-21 | Loda David C. | Engine-mounted microserver |
US20030105565A1 (en) * | 2001-12-03 | 2003-06-05 | Loda David C. | Integrated internet portal and deployed product microserver management system |
US20050027826A1 (en) * | 2001-12-03 | 2005-02-03 | Loda David C. | Microserver test port retrofit kit |
EP1540499A4 (en) * | 2002-05-21 | 2010-06-02 | Jesse Russell | ADVANCED MULTI-HOME CLIENT DEVICE FOR BROADBAND MULTIMEDIA ACCESS TO PUBLIC AND PRIVATE WIRELESS NETWORKS |
US7669237B2 (en) * | 2002-08-27 | 2010-02-23 | Trust Digital, Llc | Enterprise-wide security system for computer devices |
US7793003B2 (en) * | 2003-01-31 | 2010-09-07 | Qwest Communications International Inc | Systems and methods for integrating microservers with a network interface device |
US7376386B2 (en) * | 2003-06-02 | 2008-05-20 | Qwest Communications International Inc | Systems and methods for distributing content objects in a telecommunication system |
US7043348B2 (en) * | 2003-03-03 | 2006-05-09 | Honeywell International, Inc. | Transient fault detection system and method |
US20060155432A1 (en) * | 2005-01-07 | 2006-07-13 | United Technologies Corporation | Methods and systems for monitoring atmospheric conditions, predicting turbulent atmospheric conditions and optimizing flight paths of aircraft |
-
2004
- 2004-01-30 US US10/769,427 patent/US7167788B2/en not_active Expired - Lifetime
- 2004-10-04 NZ NZ535744A patent/NZ535744A/en unknown
- 2004-10-06 SG SG200407945A patent/SG113544A1/en unknown
- 2004-10-06 SG SG200705540-3A patent/SG134337A1/en unknown
- 2004-10-06 SG SG200705537-9A patent/SG134335A1/en unknown
- 2004-10-12 TW TW093130920A patent/TW200525367A/zh unknown
- 2004-10-27 CA CA002486088A patent/CA2486088A1/en not_active Abandoned
- 2004-11-04 AU AU2004226952A patent/AU2004226952A1/en not_active Abandoned
- 2004-11-18 EP EP04257148.9A patent/EP1562151B1/en active Active
- 2004-11-30 BR BR0405155-6A patent/BRPI0405155A/pt not_active IP Right Cessation
- 2004-12-16 MX MXPA04012874A patent/MXPA04012874A/es unknown
- 2004-12-31 CN CN2004101031554A patent/CN1649348B/zh active Active
-
2005
- 2005-01-11 JP JP2005003518A patent/JP4762556B2/ja active Active
- 2005-01-28 RU RU2005102131/09A patent/RU2005102131A/ru not_active Application Discontinuation
-
2006
- 2006-06-08 US US11/449,083 patent/US7246003B2/en not_active Expired - Lifetime
-
2007
- 2007-02-16 US US11/707,305 patent/US7251554B2/en not_active Expired - Lifetime
Non-Patent Citations (1)
Title |
---|
None * |
Also Published As
Publication number | Publication date |
---|---|
TW200525367A (en) | 2005-08-01 |
US7246003B2 (en) | 2007-07-17 |
EP1562151A3 (en) | 2005-11-16 |
BRPI0405155A (pt) | 2005-09-20 |
US7251554B2 (en) | 2007-07-31 |
RU2005102131A (ru) | 2006-07-10 |
NZ535744A (en) | 2006-06-30 |
JP2005235179A (ja) | 2005-09-02 |
SG134335A1 (en) | 2007-08-29 |
US7167788B2 (en) | 2007-01-23 |
US20060241845A1 (en) | 2006-10-26 |
JP4762556B2 (ja) | 2011-08-31 |
CN1649348B (zh) | 2012-05-23 |
SG134337A1 (en) | 2007-08-29 |
MXPA04012874A (es) | 2005-08-03 |
CA2486088A1 (en) | 2005-07-30 |
AU2004226952A1 (en) | 2005-08-18 |
EP1562151A2 (en) | 2005-08-10 |
SG113544A1 (en) | 2005-08-29 |
CN1649348A (zh) | 2005-08-03 |
US20050171651A1 (en) | 2005-08-04 |
US20070150160A1 (en) | 2007-06-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1562151B1 (en) | Dual-architecture microserver card | |
US7844385B2 (en) | Microserver engine control card | |
EP1592204A1 (en) | Engine-mounted microserver | |
EP1592203A1 (en) | Microserver test port retrofit kit | |
AU2002301638B2 (en) | Integrated internet portal and deployed product microserver management system | |
EP1679624B1 (en) | Remotely accessible integrated subsystems for parallel computing in an aircraft | |
NZ546230A (en) | An electronic controller for an engine | |
KR20070016439A (ko) | 이중 구조 마이크로서버 카드 | |
NZ546224A (en) | A method of communicating with a deployed product using a microserver card | |
KR20070016448A (ko) | 마이크로서버 엔진 제어 카드 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LU MC NL PL PT RO SE SI SK TR |
|
AX | Request for extension of the european patent |
Extension state: AL HR LT LV MK YU |
|
RTI1 | Title (correction) |
Free format text: DUAL-ARCHITECTURE MICROSERVER CARD |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LU MC NL PL PT RO SE SI SK TR |
|
AX | Request for extension of the european patent |
Extension state: AL HR LT LV MK YU |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: 7H 04L 29/06 A |
|
17P | Request for examination filed |
Effective date: 20060206 |
|
AKX | Designation fees paid |
Designated state(s): AT BE BG |
|
RBV | Designated contracting states (corrected) |
Designated state(s): DE FR GB |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: 8566 |
|
17Q | First examination report despatched |
Effective date: 20081103 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
INTG | Intention to grant announced |
Effective date: 20151002 |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: RATEZE REMOTE MGMT. L.L.C. |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
INTG | Intention to grant announced |
Effective date: 20160302 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE FR GB |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602004049274 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 13 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602004049274 Country of ref document: DE |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed |
Effective date: 20170214 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 14 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 15 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R079 Ref document number: 602004049274 Country of ref document: DE Free format text: PREVIOUS MAIN CLASS: H04L0029060000 Ipc: H04L0065000000 |
|
P01 | Opt-out of the competence of the unified patent court (upc) registered |
Effective date: 20230527 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20231013 Year of fee payment: 20 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20231010 Year of fee payment: 20 Ref country code: DE Payment date: 20231010 Year of fee payment: 20 |